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CONTINUUM DYNAMICS INC

Company Information
Address
34 LEXINGTON AVE
EWING, NJ 08618-2302
United States


http://www.continuum-dynamics.com

Information

UEI: DUE3E75K1MJ3

# of Employees: 28


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Advanced Rotorcraft Aerodynamic Modules for Flight Testing Support, Simulation and Analysis

    Amount: $829,659.00

    Accurate aerodynamic modeling is crucial to simulation, analysis and flight testing support of rotorcraft. In this regard, current analysis tools inadequately model key phenomena like blade dynamic s ...

    SBIRPhase II2006Department of Defense Navy
  2. A Self-Adaptive Refueling Drogue

    Amount: $167,175.00

    Current technology aerial refueling drogues cannot accommodate the desired range of Navy/Marine refueling missions in a single design configuration. A novel drogue design approach that incorporates a ...

    SBIRPhase II2006Department of Defense Navy
  3. High Temperature Smart Structures for Engine Noise Reduction and Performance Enhancement

    Amount: $599,832.00

    Noise mitigation for subsonic transports is a continuing high priority, and recent work has identified successful exhaust mixing enhancement devices (chevrons) that have demonstrated substantial capab ...

    SBIRPhase II2006National Aeronautics and Space Administration
  4. Novel Experimental and Numerical Methods for the Aeromechanical Design of Flapping Wing Hovering MAVs

    Amount: $99,935.00

    Recent developments have made clear the strong potential of Micro Air Vehicles (MAVs) for a wide range of surveillance and tactical reconnaissance functions, particularly if the challenging but critic ...

    STTRPhase I2006Department of Defense Air Force
  5. HALE Modeling Tools for Real Time Hardware-Coupled Aeroservoelastic Simulations

    Amount: $69,982.00

    Ongoing work under NASA sponsorship is defining promising High Altitude Long Endurance (HALE) demonstration vehicle designs for remote sensing, communication relay, environmental monitoring, and other ...

    SBIRPhase I2006National Aeronautics and Space Administration
  6. SBIR Phase II: A Novel Clamp-On Self-Powered Flowmeter

    Amount: $496,929.00

    This Small Business Innovation Research (SBIR) Phase II project will produce a prototype low-rate fluid flow instrument for nuclear power plants that incorporates several novel features that permit it ...

    SBIRPhase II2005National Science Foundation
  7. Smart Materials Technology for High Speed Adaptive Inlet/Nozzle Design

    Amount: $598,993.00

    Enabling a new generation of high-speed civil aircraft will require breakthrough developments in propulsion systems, including novel techniques to optimize inlet performance in multiple operating cond ...

    SBIRPhase II2005National Aeronautics and Space Administration
  8. Novel Eulerian Vorticity Transport Wake Module for Rotorcraft Flow Analysis

    Amount: $119,765.00

    Accurate rotorcraft performance prediction is essential to both the design and development of rotorcraft, and also the support of flight testing, establishing of safe flight envelopes and analysis of ...

    SBIRPhase I2005Department of Defense Army
  9. Rotorcraft Brownout Aerodynamic Analysis and Flight Simulation

    Amount: $119,663.00

    A critical operational problem for current Army rotorcraft is the prediction of landing conditions in a sand/dust/snow laden environment where rotorwash picks up loose ground cover leading to a condit ...

    SBIRPhase I2005Department of Defense Army
  10. Advanced Rotorcraft Brownout Aerodynamic Analysis and Flight Simulation

    Amount: $729,738.00

    A critical operational problem for Army rotorcraft is “brownout” caused by excessive dust and debris kicked up by helicopter rotorwash during take-off and landing. This can eliminate visibility a ...

    SBIRPhase II2005Department of Defense Army
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